TY - GEN
T1 - Computational Fluid Dynamics Study of Modification to Front Wing Endplate of FSAE Race Car for Drag Reduction
AU - Wu, Haowei
AU - Agarwal, Ramesh K.
N1 - Publisher Copyright:
© 2023, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2023
Y1 - 2023
N2 - This study focuses on the design and parametric optimization of the curved endplate on the front wing of a FSAE race car. ANSYS Fluent is used for mesh generation and numerical simulation. Post-processing of the results is completed in Fluent and ANSYS Ensight. By modifying the front wing endplates, outwash flow could be generated to reduce the pressure differential on the longitudinal axis of the front tire. Front tire wake could be controlled, and the drag of the car could be reduced. This study explores different configurations of the front wing endplate and aims to find the best geometry for drag reduction. Three endplate designs are considered: plain Gurney flap, Gurney flap with fillet, and angled flap with fillet. A geometry using curved endplate with Gurney flap was found to be the most effective and achieved 2.3% reduction in overall vehicle drag.
AB - This study focuses on the design and parametric optimization of the curved endplate on the front wing of a FSAE race car. ANSYS Fluent is used for mesh generation and numerical simulation. Post-processing of the results is completed in Fluent and ANSYS Ensight. By modifying the front wing endplates, outwash flow could be generated to reduce the pressure differential on the longitudinal axis of the front tire. Front tire wake could be controlled, and the drag of the car could be reduced. This study explores different configurations of the front wing endplate and aims to find the best geometry for drag reduction. Three endplate designs are considered: plain Gurney flap, Gurney flap with fillet, and angled flap with fillet. A geometry using curved endplate with Gurney flap was found to be the most effective and achieved 2.3% reduction in overall vehicle drag.
UR - http://www.scopus.com/inward/record.url?scp=85199498540&partnerID=8YFLogxK
U2 - 10.2514/6.2023-1007
DO - 10.2514/6.2023-1007
M3 - Conference contribution
AN - SCOPUS:85199498540
SN - 9781624106996
T3 - AIAA SciTech Forum and Exposition, 2023
BT - AIAA SciTech Forum and Exposition, 2023
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA SciTech Forum and Exposition, 2023
Y2 - 23 January 2023 through 27 January 2023
ER -